Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE · 2000 · 54 citations · 9 references
EngineeringAerospace EngineeringPhysicsAstrodynamicsFlight MechanicsPropulsionAir-breathing PropulsionLaser OpticsLaser PhysicsPropulsion System PerformancePropulsion SystemsRocket PropulsionCoupling CoefficientLow Earth Orbit DynamicsLow Earth OrbitsPropulsion DynamicsPropulsion System DesignPropulsion System RequirementsShock-wave InteractionThrust Analysis
Vertical flight and pendulum experiments have been carried out with a simple paraboloid type lightcraft in the air-breathing mode. Pulsed laser energy of up to 240 J/pulse was delivered from a highly reproducible e-beam sustained CO<SUB>2</SUB>-laser at repetition rates up to 45 Hz. The lightcraft mass was varied in the range between 22 and 55 g. An average thrust of 1.1 N has been derived from the flight data and the highest impulse coupling coefficient found in the pendulum experiments was 33.3(DOT)10<SUP>-5</SUP> Ns/J. A double shock wave was detected that leaves the thruster exit and an attempt was made to model the thrust, using a modification of Sedov's similarity solution for a blast wave. Finally, the propulsion requirements for the launch of a 10 kg mass into low Earth orbit are presented.
9
Similarity and Dimensional Methods in Mechanics
L. I. Sedov, Morris D. Friedman, Maurice Holt et al. · Journal of Applied Mechanics · 1961 · 935 citations · Full text
Impulse coupling to targets in vacuum by KrF, HF, and CO2 single-pulse lasers
Claude Phipps, Tom Turner, R. F. Harrison et al. · Journal of Applied Physics · 1988 · 437 citations
Propulsion to Orbit by Ground-Based Lasers
Arthur Kantrowitz · Medical Entomology and Zoology · 1972 · 228 citations
Propulsion by Absorption of Laser Radiation
A. N. Pirri, M.J. Monsler, Peter E. Nebolsine · AIAA Journal · 1974 · 97 citations